View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 42734U 98067MP 18318.24538221 .12474274 12505-4 35882-3 0 9995
2 42734 51.6055 286.4142 0002642 166.4742 193.6358 16.45390460 84235
| Epoch (UTC): | 14 November 2018 05:53:21 |
| Eccentricity: | 0.0002642 |
| inclination: | 51.6055° |
| perigee height: | 150 km |
| apogee height: | 153 km |
| right ascension of ascending node: | 286.4142° |
| argument of perigee: | 166.4742° |
| revolutions per day: | 16.45390460 |
| mean anomaly at epoch: | 193.6358° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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